LEADER 01914oam  2200541   450 
001 9910717297703321
005 20220225133249.0
035   $a(CKB)5470000002529245
035   $a(OCoLC)1158388771
035   $a(EXLCZ)995470000002529245
100   $a20200615d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe compressive yield strength of extruded shapes of 24ST aluminum alloy /$fby R.L. Templin, F.M. Howell, and E.C. Hartmann
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (11 pages, 7 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 793
300   $a"January 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 8).
606   $aAluminum alloys
606   $aMaterials$xCompression testing
606   $aStrength of materials
606   $aAluminum alloys$2fast
606   $aMaterials$xCompression testing$2fast
606   $aStrength of materials$2fast
615  0$aAluminum alloys.
615  0$aMaterials$xCompression testing.
615  0$aStrength of materials.
615  7$aAluminum alloys.
615  7$aMaterials$xCompression testing.
615  7$aStrength of materials.
700   $aTemplin$b R. L.$01423297
702   $aHowell$b F. M.
702   $aHartmann$b E. C.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717297703321
996   $aThe compressive yield strength of extruded shapes of 24ST aluminum alloy$93550453
997   $aUNINA